| 发明名称 |
SHROUDED SINGLE CRYSTAL DUAL ALLOY TURBINE DISK |
| 摘要 |
A turbine engine component for a gas turbine engine includes an inner disk, an outer shroud, and a plurality of blades. Each blade comprises a blade root and an airfoil body. The blade root is plated at least in part with a noble metal, and is coupled to the inner disk. The airfoil body extends at least partially between the blade root and the outer shroud.
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| 申请公布号 |
US2009068016(A1) |
申请公布日期 |
2009.03.12 |
| 申请号 |
US20070737949 |
申请日期 |
2007.04.20 |
| 申请人 |
HONEYWELL INTERNATIONAL, INC. |
发明人 |
PERRON JAMES S.;BAKER WILLIAM C.;RICE DEREK A. |
| 分类号 |
F01D5/14;B21D53/78;B21K3/04;B23P15/02;B23P19/04;F01D5/22;F01D5/30 |
主分类号 |
F01D5/14 |
| 代理机构 |
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代理人 |
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| 主权项 |
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